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] PERTURBING FORCES IN A CONTACTLESS ORBITAL TRANSFER SYSTEM WITH BEAM MISALIGNMENT. Spase Sciense and Technology. 2026 ;32(4):12-29.
Feed-forwardcontrol of additional deployment of a space tether with recovery of its initial vertical orientation. Space Science and Technology. 2024 ;30(5):03-18.
Feed-forward control of total retrieval of the space tether from vertical position. Space Science and Technology. 2021 ;27(5):071-085.
Expanding the flexible long element aboard spacecraft with the magnetic damper. Kosm. nauka tehnol. 2014 ;20(1):28-43.
Project “space sheppard” with ion beam. ideas and problems. Kosm. nauka tehnol. 2014 ;20(2):55–60.
The dynamics of the spacecraft with gyro-gravity stabilization in the deployment of a flexible ring antenna. Kosm. nauka tehnol. 2011 ;17(5):03-18.
The dynamics of deployment of the ring antennae on the spacecraft without stabilization. Kosm. nauka tehnol. 2009 ;15(6):57-66.
Dynamics of a deformed space system of bodies with programmed change of the configuration. Kosm. nauka tehnol. 2004 ;10(1):045-053.
Tethered satellite systems: Review of the problem. Kosm. nauka tehnol. 1997 ;3(3):021–029.